Prediction of Heat Transfer Characteristics for Discrete Hole Film Cooling - One Row of Injection Into a Turbulent Boundary Layer

Daneshmund K. Tafti,; Savash Yavuzkurt,

doi:10.1515/TJJ.1991.8.3-4.235

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Prediction of Heat Transfer Characteristics for Discrete Hole Film Cooling - One Row of Injection Into a Turbulent Boundary Layer

Daneshmund K. Tafti, and Savash Yavuzkurt,

Published/Copyright: December 1, 1991

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From the journal International Journal of Turbo and Jet Engines Volume 8 Issue 3-4

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Tafti,, Daneshmund K. and Yavuzkurt,, Savash. "Prediction of Heat Transfer Characteristics for Discrete Hole Film Cooling - One Row of Injection Into a Turbulent Boundary Layer" International Journal of Turbo and Jet Engines, vol. 8, no. 3-4, pp. 235-266. https://doi.org/10.1515/TJJ.1991.8.3-4.235

Tafti,, D. & Yavuzkurt,, S. (). Prediction of Heat Transfer Characteristics for Discrete Hole Film Cooling - One Row of Injection Into a Turbulent Boundary Layer. International Journal of Turbo and Jet Engines, 8(3-4), 235-266. https://doi.org/10.1515/TJJ.1991.8.3-4.235

Tafti,, D. and Yavuzkurt,, S. () Prediction of Heat Transfer Characteristics for Discrete Hole Film Cooling - One Row of Injection Into a Turbulent Boundary Layer. International Journal of Turbo and Jet Engines, Vol. 8 (Issue 3-4), pp. 235-266. https://doi.org/10.1515/TJJ.1991.8.3-4.235

Tafti,, Daneshmund K. and Yavuzkurt,, Savash. "Prediction of Heat Transfer Characteristics for Discrete Hole Film Cooling - One Row of Injection Into a Turbulent Boundary Layer" International Journal of Turbo and Jet Engines 8, no. 3-4 (): 235-266. https://doi.org/10.1515/TJJ.1991.8.3-4.235

Tafti, D, Yavuzkurt, S. Prediction of Heat Transfer Characteristics for Discrete Hole Film Cooling - One Row of Injection Into a Turbulent Boundary Layer. International Journal of Turbo and Jet Engines. ;8(3-4): 235-266. https://doi.org/10.1515/TJJ.1991.8.3-4.235

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Published Online: 1991-12

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Articles in the same Issue

CONTENTS
Influence of Inlet Boundary Conditions on Turbulent Flowfield Computation
Prediction of Airfoil Separated Flow Unsteady Aerodynamics
Numerical Investigation of Thrust-Reversing Nozzles
Prediction of Heat Transfer Characteristics for Discrete Hole Film Cooling - One Row of Injection Into a Turbulent Boundary Layer
System Design Aspects of Propulsion Education in Aerospace Engineering Curricula

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https://doi.org/10.1515/TJJ.1991.8.3-4.235

Articles in the same Issue

CONTENTS
Influence of Inlet Boundary Conditions on Turbulent Flowfield Computation
Prediction of Airfoil Separated Flow Unsteady Aerodynamics
Numerical Investigation of Thrust-Reversing Nozzles
Prediction of Heat Transfer Characteristics for Discrete Hole Film Cooling - One Row of Injection Into a Turbulent Boundary Layer
System Design Aspects of Propulsion Education in Aerospace Engineering Curricula